Author : A .R. Yass, Muhammad.
Engineering and Technology Journal,
2011, Volume 29, Issue 10, Pages 2013-2025
The kinematic coupling dynamic stability has been analyzed .The Laplace
transformation and the coefficient matrix determinant are used to find the rolling stability characteristic equation. The effect of parameters is investigated with different value of roll rate . It is found that the kinematics coupling or autorotation is critical at flying regime of low and high .The results can be used as real design requirements for further configuration improvements of the airplane.